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基于张量积模型变换和部分全驱动方法的四旋翼双环控制器设计

Quadrotors' double-loop controller design with tensor product model transformation and partial fully actuated method.

作者信息

Chang Fei, Kang Jia Pei, Huang Sha Ri Na, Zhao Guo Liang

机构信息

College of Electronic Information Engineering, Inner Mongolia University, Hohhot 010021, People's Republic of China; Inner Mongolia Power Group Mengdian Information and Telecommunication Co., Ltd., Inner Mongolia, Hohhot, 010020, People's Republic of China.

College of Electronic Information Engineering, Inner Mongolia University, Hohhot 010021, People's Republic of China.

出版信息

ISA Trans. 2024 Jul;150:181-197. doi: 10.1016/j.isatra.2024.05.023. Epub 2024 May 20.

Abstract

In the existing work of tensor product (TP) model transformation, the TP model transformation-based work on the quadrotor's control system design is scarce, the direct TP model transformation control strategy that applied to the quadrotor fails due to the calculation complexity, infeasibility of the huge amount of linear matrix inequalities, and the complexity of solving the linear matrix inequalities. To solve this problem, a partial TP model transformation-based double loop fuzzy controller has been studied in this work, the double-loop hybrid control scheme combines the fully actuated control method and the TP model transformation, while the fully actuated control method is used to the position subsystem control loop, and the TP model transformation based fuzzy controller is applied to the attitude control of the quadrotor. Moreover, for comparison purpose, a varying-input method based on TP model transformation is extended to the quadrotor's system control. The double-loop hybrid control scheme could also be extended with other TP model transformation based tensor sampling methods, such as, uniform sampling method and varying-input method. At last, the proposed algorithms are evaluated and compared on Parrot Mambo Minidrone, MFP450 and CUAV V5+ based hexarotor.

摘要

在现有的张量积(TP)模型变换工作中,基于TP模型变换的四旋翼控制系统设计工作较少,应用于四旋翼的直接TP模型变换控制策略因计算复杂度、大量线性矩阵不等式的不可行性以及求解线性矩阵不等式的复杂性而失败。为了解决这个问题,本文研究了一种基于部分TP模型变换的双环模糊控制器,该双环混合控制方案将全驱动控制方法与TP模型变换相结合,其中全驱动控制方法用于位置子系统控制回路,基于TP模型变换的模糊控制器应用于四旋翼的姿态控制。此外,为了进行比较,将基于TP模型变换的变输入方法扩展到四旋翼系统控制中。双环混合控制方案还可以用其他基于TP模型变换的张量采样方法进行扩展,如均匀采样方法和变输入方法。最后,在基于Parrot Mambo Minidrone、MFP450和CUAV V5 +的六旋翼上对所提出的算法进行了评估和比较。

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